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    • 1. 发明专利
    • C/c composite and method of manufacturing the same
    • C / C复合材料及其制造方法
    • JP2004323273A
    • 2004-11-18
    • JP2003118295
    • 2003-04-23
    • Ihi Aerospace Co Ltd株式会社アイ・エイチ・アイ・エアロスペース
    • SUZUKI SHIGERUYAMAUCHI HIROSHINOGUCHI MASASHI
    • B64G1/58C04B35/52C04B35/83
    • PROBLEM TO BE SOLVED: To provide a more densified C/C composite and a method of manufacturing the same by which the number of repeating cycle in manufacture and a production cost are reduced without using a hot isotactic pressing (HIP). SOLUTION: The method of manufacturing the C/C composite is performed by applying a carbon black (CB) impregnation process, a pitch impregnation/firing process and a thermosetting resin impregnation/firing process to a preform composed of a carbon fiber having a three-dimensional network structure at least once and densifying the surface of the preform with the thermoplastic resin after machining. The C/C composite is formed by applying the manufacturing method and using a furan resin, a phenol resin, a bis-maleimide triazine or the like as the thermosetting resin. COPYRIGHT: (C)2005,JPO&NCIPI
    • 要解决的问题:为了提供更加致密的C / C复合材料及其制造方法,通过该方法可以减少制造中的重复循环次数和生产成本,而不使用热全同立构压制(HIP)。 解决方案:制备C / C复合材料的方法是通过将炭黑(CB)浸渍工艺,沥青浸渍/焙烧工艺和热固性树脂浸渍/烧制方法应用于由具有 至少一次三维网状结构,并在加工后用热塑性树脂使预成型体的表面致密化。 通过应用制造方法并使用呋喃树脂,酚醛树脂,双马来酰亚胺三嗪等作为热固性树脂,形成C / C复合体。 版权所有(C)2005,JPO&NCIPI